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RD-851
Yuzhnoye Nitric acid/UDMH rocket engine. R-16 (SS-7) stage 1 attitude control engine . Out of Production. Four thrusters are each gimbaled in one single axis.

AKA: 8D63. Status: Out of Production. Date: 1958-63. Thrust: 32.48 kN (7,302 lbf). Unfuelled mass: 403 kg (888 lb). Specific impulse: 279 s. Specific impulse sea level: 243 s. Burn time: 115 s. Height: 1.70 m (5.50 ft). Diameter: 3.54 m (11.61 ft).

Chambers: 4. Engine: 403 kg (888 lb). Chamber Pressure: 66.20 bar. Propellant Formulation: AK27/UDMH. Thrust to Weight Ratio: 8.21. Oxidizer to Fuel Ratio: 2.45.



Subtopics

RD-852 Yuzhnoye Nitric acid/UDMH rocket engine. R-16 (SS-7) stage 2 attitude control engine. Out of Production. Four thrusters are each gimbaled in one single axis.

Family: Storable liquid. Country: Ukraine. Launch Vehicles: R-16. Propellants: Nitric acid/UDMH. Agency: Yuzhnoye. Bibliography: 344, 348.

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